RU2010109869A - DISTRIBUTED ARCHITECTURE FOR RADIO NAVIGATION EQUIPMENT - Google Patents

DISTRIBUTED ARCHITECTURE FOR RADIO NAVIGATION EQUIPMENT Download PDF

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Publication number
RU2010109869A
RU2010109869A RU2010109869/07A RU2010109869A RU2010109869A RU 2010109869 A RU2010109869 A RU 2010109869A RU 2010109869/07 A RU2010109869/07 A RU 2010109869/07A RU 2010109869 A RU2010109869 A RU 2010109869A RU 2010109869 A RU2010109869 A RU 2010109869A
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RU
Russia
Prior art keywords
receivers
aircraft
transmitters
architecture according
communication lines
Prior art date
Application number
RU2010109869/07A
Other languages
Russian (ru)
Other versions
RU2483443C2 (en
Inventor
Ален БИБО (FR)
Ален БИБО
Original Assignee
Таль (Fr)
Таль
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Таль (Fr), Таль filed Critical Таль (Fr)
Publication of RU2010109869A publication Critical patent/RU2010109869A/en
Application granted granted Critical
Publication of RU2483443C2 publication Critical patent/RU2483443C2/en

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/74—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
    • G01S13/76—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted
    • G01S13/78—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted discriminating between different kinds of targets, e.g. IFF-radar, i.e. identification of friend or foe
    • G01S13/785—Distance Measuring Equipment [DME] systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/882—Radar or analogous systems specially adapted for specific applications for altimeters
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13—Receivers
    • G01S19/35—Constructional details or hardware or software details of the signal processing chain
    • G01S19/36—Constructional details or hardware or software details of the signal processing chain relating to the receiver frond end
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/003—Transmission of data between radar, sonar or lidar systems and remote stations
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/18502—Airborne stations
    • H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Signal Processing (AREA)
  • Electromagnetism (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Optical Communication System (AREA)
  • Radio Relay Systems (AREA)

Abstract

1. Распределенная архитектура для комплекса средств обеспечения воздушной навигации летательного аппарата, отличающаяся тем, что, по меньшей мере, часть передатчиков и/или приемников (16, 39, 40) вынесены ближе к соответствующим антеннам (14, 36, 37), и тем, что эти вынесенные передатчики и/или приемники соединены линиями (15, 25, 41) цифровой связи с компьютером (21) электронной стойки (35) летательного аппарата. ! 2. Архитектура по п.1, отличающаяся тем, что, по меньшей мере, часть силового питания приборов летательного аппарата поступает от централизованного источника (23) питания, и этот централизованный источник питания распределяет (26) между вынесенными приборами питание стабилизированным постоянным током. ! 3. Архитектура по п.1 или 2, отличающаяся тем, что линии цифровой связи являются оптическими шинами. ! 4. Архитектура по п.1 или 2, отличающаяся тем, что, по меньшей мере, часть передатчиков и/или приемников (40) встроена в соответствующую антенну (37). 1. Distributed architecture for a complex of means for providing air navigation of an aircraft, characterized in that at least a portion of the transmitters and / or receivers (16, 39, 40) are brought closer to the corresponding antennas (14, 36, 37), and that these remote transmitters and / or receivers are connected by digital communication lines (15, 25, 41) to a computer (21) of the electronic rack (35) of the aircraft. ! 2. Architecture according to claim 1, characterized in that at least a portion of the power supply of the aircraft devices comes from a centralized power source (23), and this centralized power source distributes (26) stabilized direct current power between the remote devices. ! 3. The architecture according to claim 1 or 2, characterized in that the digital communication lines are optical buses. ! 4. Architecture according to claim 1 or 2, characterized in that at least a portion of the transmitters and / or receivers (40) is integrated in the corresponding antenna (37).

Claims (4)

1. Распределенная архитектура для комплекса средств обеспечения воздушной навигации летательного аппарата, отличающаяся тем, что, по меньшей мере, часть передатчиков и/или приемников (16, 39, 40) вынесены ближе к соответствующим антеннам (14, 36, 37), и тем, что эти вынесенные передатчики и/или приемники соединены линиями (15, 25, 41) цифровой связи с компьютером (21) электронной стойки (35) летательного аппарата.1. Distributed architecture for a complex of means for providing air navigation of an aircraft, characterized in that at least a portion of the transmitters and / or receivers (16, 39, 40) are brought closer to the corresponding antennas (14, 36, 37), and that these remote transmitters and / or receivers are connected by digital communication lines (15, 25, 41) to a computer (21) of the electronic rack (35) of the aircraft. 2. Архитектура по п.1, отличающаяся тем, что, по меньшей мере, часть силового питания приборов летательного аппарата поступает от централизованного источника (23) питания, и этот централизованный источник питания распределяет (26) между вынесенными приборами питание стабилизированным постоянным током.2. Architecture according to claim 1, characterized in that at least a portion of the power supply of the aircraft devices comes from a centralized power source (23), and this centralized power source distributes (26) stabilized direct current power between the remote devices. 3. Архитектура по п.1 или 2, отличающаяся тем, что линии цифровой связи являются оптическими шинами.3. The architecture according to claim 1 or 2, characterized in that the digital communication lines are optical buses. 4. Архитектура по п.1 или 2, отличающаяся тем, что, по меньшей мере, часть передатчиков и/или приемников (40) встроена в соответствующую антенну (37). 4. Architecture according to claim 1 or 2, characterized in that at least a portion of the transmitters and / or receivers (40) is integrated in the corresponding antenna (37).
RU2010109869/07A 2007-08-17 2008-08-14 Distributed architecture for radio navigation equipment RU2483443C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0705886A FR2920062B1 (en) 2007-08-17 2007-08-17 ARCHITECTURE DISTRIBUTED FOR ALL RADIONAVIGATION AID
FR0705886 2007-08-17
PCT/EP2008/060701 WO2009024532A1 (en) 2007-08-17 2008-08-14 Distributed architecture for all radio navigation aids

Publications (2)

Publication Number Publication Date
RU2010109869A true RU2010109869A (en) 2011-09-27
RU2483443C2 RU2483443C2 (en) 2013-05-27

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010109869/07A RU2483443C2 (en) 2007-08-17 2008-08-14 Distributed architecture for radio navigation equipment

Country Status (6)

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US (1) US8437888B2 (en)
EP (1) EP2176962B1 (en)
CA (1) CA2696574A1 (en)
FR (1) FR2920062B1 (en)
RU (1) RU2483443C2 (en)
WO (1) WO2009024532A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140032002A1 (en) 2012-07-30 2014-01-30 The Boeing Company Electric system stabilizing system for aircraft
US9118112B1 (en) 2013-03-14 2015-08-25 Rockwell Collins, Inc. Multi-sensor system and method for vehicles
EP3298855B1 (en) * 2015-05-19 2018-08-29 Telefonaktiebolaget LM Ericsson (publ) Methods, wireless communication device and radio network node for managing contention resolution
US10425150B1 (en) * 2016-07-19 2019-09-24 Rockwell Collins, Inc. Remotely-managed aircraft RF communication network, device, and method
CN110783693A (en) * 2019-10-12 2020-02-11 中航通飞研究院有限公司 Antenna layout method based on amphibious aircraft

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8081968B2 (en) * 2000-10-11 2011-12-20 Gogo Llc System for creating an air-to-ground IP tunnel in an airborne wireless cellular network to differentiate individual passengers
FR2731799B1 (en) * 1995-03-13 1997-06-20 Concept Aero System Sarl Soc METHOD AND DEVICE FOR ANALYZING RADIONAVIGATION SIGNALS
GB2310114A (en) * 1996-02-08 1997-08-13 Gec-Marconi Limited Data distribution systems in vehicles
JP3024569B2 (en) * 1996-09-20 2000-03-21 日本電気株式会社 Electrical connection structure between planar antenna and transceiver
FR2787658B1 (en) * 1998-12-18 2001-03-16 Sextant Avionique COMMUNICATION MODES MANAGEMENT METHOD FOR AN AIRCRAFT
US6477152B1 (en) * 1998-12-30 2002-11-05 Honeywell Inc. Apparatus and method for data communications
US7177939B2 (en) * 1999-05-14 2007-02-13 Cingular Wireless Ii, Llc Aircraft data communications services for users
US20020045974A1 (en) * 2000-05-12 2002-04-18 Stephen Heppe Dual-band radio communications system for aeronautical data communications
JP3641582B2 (en) * 2000-10-27 2005-04-20 日本無線株式会社 ADE unit for AIS
FR2819964B1 (en) * 2001-01-23 2003-04-11 Thomson Csf METHOD FOR SELECTING ACTIVABLE APPLICATIONS THROUGH A CIVIL AERONAUTICAL COMMUNICATION NETWORK
TWI266451B (en) * 2002-07-24 2006-11-11 Yageo Corp Integrated antenna for portable computer
US7177638B2 (en) * 2004-12-28 2007-02-13 Live Tv, Llc Aircraft in-flight entertainment system including digital radio service and associated methods

Also Published As

Publication number Publication date
FR2920062A1 (en) 2009-02-20
US8437888B2 (en) 2013-05-07
FR2920062B1 (en) 2015-01-30
US20110022249A1 (en) 2011-01-27
EP2176962A1 (en) 2010-04-21
WO2009024532A1 (en) 2009-02-26
RU2483443C2 (en) 2013-05-27
CA2696574A1 (en) 2009-02-26
EP2176962B1 (en) 2016-08-03

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Effective date: 20140815